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    題名: Missile Guidance Using Dual-Mode Seeker
    作者: Ma, Der-Ming;Shiau, Jaw-Kuen;Ho, Ian
    貢獻者: 淡江大學航空太空工程學系
    關鍵詞: Dual-mode seeker guidance;IR seeker;Kalman filter;Proportional navigation;RF seeker
    日期: 2011-08
    上傳時間: 2013-03-20 16:36:41 (UTC+8)
    出版者: Manchester: Scholarlink Resource Centre Ltd.
    摘要: This study developed an analytical method to quantitatively analyze the dual-mode seeker guidance performance. The method derives the seekers' measurement models and implements the Kalman filter. The study takes the RF/IR dual-mode seeker, which is proposed for advanced long/medium range air-to-air missiles, as the example. The two-dimensional guidance loop is used to illustrate the methodology and dimensionless equations are derived for generality. After discussing several missile-target scenarios, the results show that the developed scheme provides sufficiently accurate target information for missile guidance, not only for dual-mode seekers, but also when one of the seekers is jammed. The methodology developed in the study can also be applied to increase the accuracy of target tracking.
    關聯: Journal of Emerging Trends in Engineering and Applied Sciences 2(4), pp.636-642
    顯示於類別:[航空太空工程學系暨研究所] 期刊論文

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